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Thermally isolated deployable shield for spacecraftA thermally isolated deployable shield for spacecraft is provided utilizing a plurality of lattice panels stowable generally against the craft and deployable to some fixed distance from the craft. The lattice panels are formed from replaceable shield panels affixed to lattice structures. The lattice panels generally encircle the craft providing 360 degree coverage therearound. Actuation means are provided from translating the shield radially outward from the craft and thermally isolating the shield from the craft. The lattice panels are relatively flexible, allowing the shield to deploy to variable diameters while retaining uniform curvature thereof. Restraining means are provided for holding the shield relatively tight in its stowed configuration. Close-out assemblies provide light sealing and protection of the annular spaces between the deployed shield and the crafts end structure.
Document ID
19910015853
Acquisition Source
Legacy CDMS
Document Type
Other - Patent Application
Authors
Redmon, John W., Jr.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Miller, Andre E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lawson, Bobby E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Cobb, William E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
April 18, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.71:MFS-28524-1
Patent Application Number: US-PATENT-APPL-SN-691610
Report Number: NAS 1.71:MFS-28524-1
Patent Number: NASA-CASE-MFS-28524-1
Accession Number
91N25167
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MFS-28524-1
Patent Application
US-PATENT-APPL-SN-691610
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